Active Control Law Design for Flutter/LCO Suppression Based on Reduced Order Model Method
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference17 articles.
1. Reduced-order modeling: new approaches for computational physics;Lucia;Progress in Aerospace Sciences,2004
2. Silva W A. identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques. AIAA-1997-3712, 1997.
3. Volterra series based transonic unsteady aerodynamics modeling;Wu;Journal of Beijing University of Aeronautics and Astronautics,2006
4. Gupta K K, Voelker L S, Bach C, et al. CFD-based aeroelastic analysis of the X-43 hypersonic flight vehicle. AIAA-2001-712, 2001.
5. Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows;Hall;AIAA Journal,2000
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